EP2940859B1 - Module d'estimation d'angle de rotation pour commande vectorielle sans capteur de pmsm - Google Patents

Module d'estimation d'angle de rotation pour commande vectorielle sans capteur de pmsm Download PDF

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EP2940859B1
EP2940859B1 EP15163779.0A EP15163779A EP2940859B1 EP 2940859 B1 EP2940859 B1 EP 2940859B1 EP 15163779 A EP15163779 A EP 15163779A EP 2940859 B1 EP2940859 B1 EP 2940859B1
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Prior art keywords
flux
fixed
coordinate system
axis
rotation angle
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German (de)
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EP2940859A1 (fr
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Kwang Woon Kim
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LS Electric Co Ltd
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LSIS Co Ltd
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    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02P—CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
    • H02P21/00—Arrangements or methods for the control of electric machines by vector control, e.g. by control of field orientation
    • H02P21/14—Estimation or adaptation of machine parameters, e.g. flux, current or voltage
    • H02P21/141—Flux estimation
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02P—CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
    • H02P6/00—Arrangements for controlling synchronous motors or other dynamo-electric motors using electronic commutation dependent on the rotor position; Electronic commutators therefor
    • H02P6/14—Electronic commutators
    • H02P6/16—Circuit arrangements for detecting position
    • H02P6/18—Circuit arrangements for detecting position without separate position detecting elements
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02P—CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
    • H02P21/00—Arrangements or methods for the control of electric machines by vector control, e.g. by control of field orientation
    • H02P21/14—Estimation or adaptation of machine parameters, e.g. flux, current or voltage
    • H02P21/18—Estimation of position or speed
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02P—CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
    • H02P31/00—Arrangements for regulating or controlling electric motors not provided for in groups H02P1/00 - H02P5/00, H02P7/00 or H02P21/00 - H02P29/00

Definitions

  • the present disclosure relates to a sensorless vector control system of a permanent magnet synchronous motor (PMSM), and more particularly, to a rotation angle estimation module for sensorless vector control of a PMSM.
  • PMSM permanent magnet synchronous motor
  • a separate location sensor such as an encoder or resolver is used for detecting the location.
  • a sensor less control method may estimate information on the speed and location of the rotor without installing a separate location sensor.
  • Typical sensorless vector control methods of a PMSM include a method of using counter electromotive force, a method of using a voltage model, a method of using a model reference controller, a method of using a status estimation module, a Kalman filter, non-linear control, and intellectual control, but since they need a significant amount of calculation and an estimation error occurs in a low-speed region, there was a limitation in that they are not easy to actually use.
  • Korean Patent Nos. 1025640 and 0845110 Korean Patent Laid-Open Publication No. 2010-0058905 , etc. are found as arts related to sensorless vector control of a motor, but they are not related to the control method of the PMSM and irrelevant to the present invention that intends to decrease the amount of calculation and increase accuracy.
  • US 2013/093370 A1 discloses a parameter estimating apparatus for permanent magnet synchronous motor driving system is disclosed, the apparatus estimating an inductance and a magnet flux linkage of a permanent magnet through a real-time magnetic flux estimation, whereby an operation performance of the PMSM can be enhanced.
  • Embodiments provide a rotation angle estimation module and a sensorless vector control system of a permanent magnet synchronous motor (PMSM) employing the module that decrease an amount of calculation for the rotation angle estimation of the PMSM and minimize an estimation error, in the sensorless vector control of the PMSM.
  • PMSM permanent magnet synchronous motor
  • a rotation angle estimation module of a permanent magnetic synchronous motor (PMSM) for sensorless vector control of the PMSM includes: a fixed flux instruction estimation unit calculating a rotating flux ( ⁇ sd , ⁇ sq ) and a fixed flux instruction ( ⁇ s ⁇ *, ⁇ s ⁇ *) based on a rotation angle ⁇ and the current (I s ⁇ , I s ⁇ ) of a fixed coordinate system; a fixed flux estimation unit calculating a fixed flux ( ⁇ s ⁇ , ⁇ s ⁇ ) based on the voltage (V s ⁇ , V s ⁇ ) of the fixed coordinate system, and the current (I s ⁇ , I s ⁇ ) and fixed flux error ( ⁇ s ⁇ , ⁇ s ⁇ ) of the fixed coordinate system; a fixed flux error estimation unit using the difference between the fixed flux instruction ( ⁇ s ⁇ *, ⁇ s ⁇ *) and the fixed flux ( ⁇ s ⁇ , ⁇ s ⁇ ) to calculate the fixed flux error ( ⁇
  • the trigonometric function calculation unit may finally calculate the rotation angle ⁇ and feeds a calculated angle back to the fixed flux instruction estimation unit.
  • the fixed flux instruction estimation unit may calculate the rotating flux ( ⁇ sd , ⁇ sq ) based on the current (I s ⁇ , I s ⁇ ) of the fixed coordinate system, the rotation angle ⁇ , the inductance (L d , L q ) of a rotary coordinate system, and the flux ⁇ PM of a permanent magnet.
  • the fixed flux instruction estimation unit may compensate for the rotation angle ⁇ by using the rotating flux ( ⁇ sd , ⁇ sq ) to calculate a fixed flux instruction ( ⁇ s ⁇ *, ⁇ s ⁇ *).
  • the fixed flux error estimation unit may calculate the difference between the ⁇ axis flux instruction value ⁇ s ⁇ * of the fixed coordinate system input from the fixed flux instruction estimation unit and the ⁇ axis flux ⁇ s ⁇ input from the fixed flux estimation unit, calculate the difference between the ⁇ axis flux instruction value ⁇ s ⁇ * of the fixed coordinate system input from the fixed flux instruction estimation unit and the ⁇ axis flux ⁇ s ⁇ input from the fixed flux estimation unit, receive the difference from the ⁇ axis flux ⁇ s ⁇ to adjust a gain and calculate the ⁇ axis flux error ⁇ s ⁇ of the fixed coordinate system, and receive the difference from the ⁇ axis flux ⁇ s ⁇ to adjust a gain and calculate the ⁇ axis flux error ⁇ s ⁇ of the fixed coordinate system.
  • the trigonometric function calculation unit 40 may find angles ⁇ dq and ⁇ ⁇ by the applying of a trigonometric function to the rotating flux ( ⁇ sd , ⁇ sq ) and the fixed flux ( ⁇ s ⁇ , ⁇ s ⁇ ), respectively, and output the rotation angle ⁇ based on the angles ⁇ dq and ⁇ ⁇ .
  • the trigonometric function calculation unit 40 may receive the d axis flux ⁇ sd of the rotary coordinate system and the q axis flux ⁇ sq of the rotary coordinate system from the fixed flux instruction estimation unit to output the angle ⁇ dq of ⁇ dq based on the d axis by using a trigonometric function arctangent, receive the ⁇ axis flux ⁇ s ⁇ of the fixed coordinate system and the ⁇ axis flux ⁇ s ⁇ of the fixed coordinate system from the fixed flux estimation unit to output the angle ⁇ ⁇ of ⁇ ⁇ based on the ⁇ axis by using the trigonometric function arctangent, and find the difference between the angles ⁇ dq and ⁇ ⁇ to output the rotation angle ⁇ .
  • an operating method of a rotation angle estimation module of a motor for sensorless vector control of a PMSM includes: calculating a rotating flux ( ⁇ sd , ⁇ sq ) and a fixed flux instruction ( ⁇ s ⁇ *, ⁇ s ⁇ *) based on the current (I s ⁇ , I s ⁇ ) of a fixed coordinate system and a rotation angle ⁇ ; calculating a fixed flux ( ⁇ s ⁇ , ⁇ s ⁇ ) based on the voltage (V s ⁇ , V s ⁇ ) of the fixed coordinate system, and the current (I s ⁇ , I s ⁇ ) and fixed flux error ( ⁇ s ⁇ , ⁇ s ⁇ ) of the fixed coordinate system, through a fixed flux estimation unit; using the difference between the fixed flux instruction ( ⁇ s ⁇ *, ⁇ s ⁇ *) and the fixed flux ( ⁇ s ⁇ , ⁇ s ⁇ ) to calculate the fixed flux error ( ⁇ s ⁇ , ⁇ s ⁇ ) and feed the errors
  • Fig. 1 shows the principle of the sensorless vector control method of a permanent magnet synchronous motor (PMSM) according to an embodiment, by using a vector diagram.
  • PMSM permanent magnet synchronous motor
  • the vector control method divides and controls currents applied to the motor into a flux current Id se and a torque current Iq se based on a rotary coordinate system.
  • the vector control method of the PMSM fixes the flux current Id se to match a rotor location ⁇ , and applies the torque current Iq se to the sensorless vector control of the PMSM.
  • Fig. 1 represents a flux relationship according to a fixed coordinate system ⁇ and a rotary coordinate system dq in the vector control of the PMSM, an axis used for a vector control system is divided into the fixed coordinate system and the rotary coordinate system, the fixed coordinate system indicates a coordinate system having a coordinate axis not rotating but fixed, and the rotary coordinate system indicates a coordinate system that rotates at any angular velocity ⁇ .,
  • An embodiment estimates a final rotor location by using stator flux vector ⁇ ⁇ based on the fixed coordinate system ⁇ and rotor flux vector ⁇ dq based on the rotary coordinate system dq along with arctangent tan -1 and information on the estimated rotor location matches the location of an actual motor.
  • Fig. 2 shows a rotation angle estimation unit 100 estimating a rotation angle ⁇ , a distance that a rotor moves, based on the vector diagram of FIG. 1 and the rotation angle estimation unit 100 includes a fixed flux instruction estimation unit 10, a fixed flux estimation unit 20, a fixed flux error estimation unit 30, and a trigonometric function calculation unit 40.
  • the fixed flux instruction estimation unit 10 calculates a rotating flux ( ⁇ s ⁇ , ⁇ sq ) and a fixed flux instruction ( ⁇ s ⁇ *, ⁇ s ⁇ *) based on the current (I s ⁇ , I s ⁇ ) and the rotation angle ⁇ based on the fixed coordinate system ⁇ .
  • the fixed flux instruction estimation unit 10 receives the current (I s ⁇ , I s ⁇ ) and rotation angle ⁇ of the fixed coordinate system ⁇ and uses a rotor flux equation to calculate the fixed flux instruction ( ⁇ s ⁇ *, ⁇ s ⁇ *).
  • the rotor flux equation firstly calculates a rotating flux ( ⁇ sd , ⁇ sq ) and finally calculates the fixed flux instruction ( ⁇ s ⁇ *, ⁇ s ⁇ *) by using a calculation result.
  • the fixed flux estimation unit 20 calculates the fixed flux ( ⁇ s ⁇ , ⁇ s ⁇ ) based on the voltage (V s ⁇ , V s ⁇ ) of the fixed coordinate system ⁇ , and the current (I s ⁇ , I s ⁇ ) and fixed flux error ( ⁇ s ⁇ , ⁇ s ⁇ ) of the fixed coordinate system.
  • the fixed flux estimation unit 20 receives the voltage (V s ⁇ , V s ⁇ ) of the fixed coordinate system ⁇ , and the current (I s ⁇ , I s ⁇ ) and fixed flux error ( ⁇ s ⁇ , ⁇ s ⁇ ) of the fixed coordinate system ⁇ and uses a stator voltage equation to calculate the fixed flux ( ⁇ s ⁇ , ⁇ s ⁇ ) of the ⁇ and ⁇ axes.
  • the fixed flux error estimation unit 30 uses the difference between the fixed flux instruction ( ⁇ s ⁇ *, ⁇ s ⁇ *) and the fixed flux ( ⁇ s ⁇ , ⁇ s ⁇ ) to calculate the fixed flux error ( ⁇ s ⁇ , ⁇ s ⁇ ) and feeds the errors back to the fixed flux estimation unit.
  • the fixed flux error estimation unit 30 uses the difference between the fixed flux instruction ( ⁇ s ⁇ *, ⁇ s ⁇ *) output by the fixed flux instruction estimation unit 10 and the fixed flux ( ⁇ s ⁇ , ⁇ s ⁇ ) output by the fixed flux estimation unit 20 to calculate the fixed flux error ( ⁇ s ⁇ , ⁇ s ⁇ ) of the ⁇ and ⁇ axes and feeds the errors back to the fixed flux estimation unit 20.
  • the trigonometric function calculation unit 40 calculates the rotation angle ⁇ , a distance that a rotor moves, based on the rotating flux ( ⁇ sd , ⁇ sq ) and the fixed flux ( ⁇ s ⁇ , ⁇ s ⁇ ).
  • the trigonometric function calculation unit 40 performs calculation on the rotating flux ( ⁇ sd , ⁇ sq ) firstly calculated by the rotor flux equation of the fixed flux instruction estimation unit 10 and the fixed flux ( ⁇ s ⁇ , ⁇ s ⁇ ) output by the fixed flux estimation unit 20 by using trigonometric functions to find angles ⁇ dq and ⁇ ⁇ , respectively.
  • the rotation angle estimation unit 100 continues to calculate the rotation angle ⁇ by feedback between the fixed flux error estimation unit 30 and the fixed flux estimation unit 20, between the fixed flux estimation unit 20 and the trigonometric function calculation unit 40, and between the fixed flux instruction estimation unit 10 and the trigonometric function calculation unit 40.
  • FIG. 3 is a block diagram representing a particular circuit configuration of the rotation angle estimation unit 100.
  • the fixed flux instruction estimation unit 10 includes a first rotary coordinate conversion unit 101, a second rotary coordinate conversion unit 102, a first rotating flux calculation unit 103, a second rotating flux calculation unit 104, a first fixed coordinate conversion unit 105, and a second fixed coordinate conversion unit 106.
  • the first rotary coordinate conversion unit 101 receives the ⁇ axis current I s ⁇ of the fixed coordinate system and the rotation angle ⁇ in order to use a rotor flux equation and coordinate-converts into the d axis current value I sd of the rotary coordinate system.
  • the second rotary coordinate conversion unit 102 receives the ⁇ axis current I s ⁇ of the fixed coordinate system and the rotation angle ⁇ and coordinate-converts into the q axis current value I sq of the rotary coordinate system.
  • the d axis flux ⁇ sd and q axis flux ⁇ sq of the rotary coordinate system are input to the trigonometric function calculation unit 40.
  • the first fixed coordinate conversion unit 105 is a compensator compensating for a value coordinate-converted in order to use the rotor flux equation, compensates for the rotation angle ⁇ by using the output of the first rotating flux calculation unit 103 to coordinate-convert into the fixed coordinate system, and outputs the ⁇ axis flux instruction value ⁇ s ⁇ * of the fixed coordinate system.
  • the second fixed coordinate conversion unit 106 compensates for the rotation angle ⁇ by using the output of the second rotating flux calculation unit 104 to coordinate-convert into the fixed coordinate system, and outputs the ⁇ axis flux instruction value ⁇ s ⁇ * of the fixed coordinate system.
  • the fixed flux estimation unit 20 includes a first fixed flux change ratio calculation unit 201, a second fixed flux change ratio calculation unit 202, a first integrator 203, and a second integrator 204.
  • the first integrator 203 integrates the outputs of the first fixed flux change ratio calculation unit 201 to output the ⁇ axis flux ⁇ s ⁇ of the fixed coordinate system.
  • the second integrator 204 integrates the outputs of the second fixed flux change ratio calculation unit 202 to output the ⁇ axis flux ⁇ s ⁇ of the fixed coordinate system.
  • the ⁇ axis flux ⁇ s ⁇ and ⁇ axis flux ⁇ s ⁇ output by the first integrator 203 and the second integrator 204 are input to the trigonometric function calculation unit 40.
  • the fixe flux error estimation unit 30 includes a first subtractor 301, a second subtractor 302, a first controller 303 and a second controller 304 and performs the function of compensating for the estimated fixed coordinate system ⁇ - ⁇ axis flux, and an error is compensated for by a PI controller and input to the fixed flux estimation unit 20.
  • the first subtractor 301 calculates the difference between the ⁇ axis flux instruction value ⁇ s ⁇ * of the fixed coordinate system input from the fixed flux instruction estimation unit 10 and the ⁇ axis flux ⁇ s ⁇ input from the fixed flux estimation unit 20.
  • the second subtractor 302 calculates the difference between the ⁇ axis flux instruction value ⁇ s ⁇ * of the fixed coordinate system input from the fixed flux instruction estimation unit 10 and the ⁇ axis flux ⁇ s ⁇ input from the fixed flux estimation unit 20.
  • the first controller 303 receives the difference from the first subtractor 301, performs proportional-integral (PI) control by the equation K P ⁇ + K I ⁇ /S (K P ⁇ : proportional gain, K I ⁇ : integral gain, S: complex variable) to adjust a gain and calculates the ⁇ axis flux error ⁇ s ⁇ of the fixed coordinate system.
  • PI proportional-integral
  • the second controller 304 receives the difference from the second subtractor 302, performs PI control by the equation K P ⁇ + K I ⁇ /S (K P ⁇ : proportional gain, K I ⁇ : integral gain, S: complex variable) to adjust a gain and calculates the ⁇ axis flux error ⁇ s ⁇ of the fixed coordinate system.
  • the ⁇ axis flux error ⁇ s ⁇ and ⁇ axis flux error ⁇ s ⁇ are fed back to the fixe flux estimation unit 20.
  • the trigonometric function calculation unit 40 includes a first arctangent unit 401, a second arctangent unit 402, and a rotation angle subtraction unit 403.
  • the first arctangent unit 401 receives the d axis flux ⁇ sd of the rotary coordinate system and the q axis flux ⁇ sq of the rotary coordinate system from the fixed flux instruction estimation unit 10 and outputs the angle ⁇ dq of ⁇ dq based on the d axis by using a trigonometric function arctangent.
  • the second arctangent unit 402 receives the ⁇ axis flux ⁇ s ⁇ of the fixed coordinate system and the ⁇ axis flux ⁇ s ⁇ of the fixed coordinate system from the fixed flux estimation unit 20 and outputs the angle ⁇ ⁇ of ⁇ ⁇ based on the ⁇ axis by using the trigonometric function arctangent.
  • the rotation angle subtraction unit 403 finds the difference between the angles ⁇ ⁇ and ⁇ dq to output the rotation angle ⁇ , and the rotation angle ⁇ is fed back to the fixed flux instruction estimation unit 10.
  • the sensorless vector control system of the PMSM receives the rotation angle ⁇ and the speed W e from the rotation angle estimation unit 100 and controls the PMSM.
  • Fig. 4 is a block diagram representing a state in which the rotation angle estimation unit 100 according to an embodiment is applied to a sensorless vector control system inverter-controlling a typical PMSM, through which it is possible to understand how the outputs of the rotation angle estimation unit 100, the rotation angle ⁇ and the speed W e are input to a PMSM control unit 1.
  • the technical scope of an embodiment includes the sensorless vector control system of the PMSM to which the rotation angle estimation unit 100 is applied.
  • the embodiment describes a method of finding the stator flux vector and the rotor flux vector, the flux equation of a rotor circuit is coordinate-converted into the stator flux equation by the applying of the voltage equation of a stator circuit and the flux equation of the rotor circuit and then the stator flux vector is compensated for to finally find the stator flux vector and the rotor flux vector.
  • the rotation angle estimation unit 100 may also be applied to a vector control system having location and speed sensors as a backup in addition to the sensorless vector control system of the PMSM.
  • stator voltage equation and the rotor equation are together used, it is possible to rapidly and accurately estimate the rotation angle of a rotor at low and high speeds and by applying the estimated rotation angle to perform the sensorless vector control of the PMSM, it is possible to provide a more reliable and economical sensorless vector control system of the PMSM.

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  • Power Engineering (AREA)
  • Control Of Ac Motors In General (AREA)
  • Control Of Motors That Do Not Use Commutators (AREA)

Claims (15)

  1. Un module d'estimation d'angle de rotation (100) d'un moteur synchrone à aimant permanent (PMSM) pour le contrôle vectoriel sans capteur du PMSM, le module d'estimation d'angle de rotation comprenant :
    une unité d'estimation de consigne de flux fixe (10) configurée pour calculer un flux tournant (λsd, λsq) et une consigne de flux fixe (λsα*, λsβ*) sur la base d'un angle de rotation (θ) et du courant (Isα, Isβ) d'un système de coordonnées fixe ;
    une unité d'estimation de flux fixe (20) configurée pour calculer un flux fixe (λsα, λsβ) sur la base de la tension (Vsα, Vsβ) du système de coordonnées fixe, et du courant (Isα, Isβ) et d'une erreur de flux fixe (Δsα, Δsβ) du système de coordonnées fixe ;
    une unité d'estimation d'erreur de flux fixe (30) configurée pour utiliser la différence entre la consigne de flux fixe (λsα*, λsβ*) et le flux fixe (λsα, λsβ) pour calculer l'erreur de flux fixe (Δsα, Δsβ) et envoyer les erreurs en retour à l'unité d'estimation de flux fixe (20) ; et
    une unité de calcul de fonction trigonométrique configurée pour calculer l'angle de rotation (θ) d'une distance dont se déplace un rotor, sur la base du flux tournant (λsd, λsq) et du flux fixe (λsα, λsβ).
  2. Le module d'estimation d'angle de rotation selon la revendication 1, dans lequel l'unité de calcul de fonction trigonométrique (40) calcule enfin l'angle de rotation θ et envoie un angle calculé en retour à l'unité d'estimation de consigne de flux fixe (10).
  3. Le module d'estimation d'angle de rotation selon la revendication 1, dans lequel l'unité d'estimation de consigne de flux fixe (10) calcule le flux tournant (λsd, λsq) sur la base du courant (Isα, Isβ) du système de coordonnées fixe, de l'angle de rotation θ, de l'inductance (Ld, Lq) d'un système de coordonnées tournant, et du flux λPM d'un aimant permanent.
  4. Le module d'estimation d'angle de rotation selon la revendication 3, dans lequel l'unité d'estimation de consigne de flux fixe (10) compense l'angle de rotation θ par utilisation du flux tournant (λsd, λsq) pour calculer la consigne de flux fixe (λsα*, λsβ*).
  5. Le module d'estimation d'angle de rotation selon la revendication 1, dans lequel l'unité d'estimation de flux fixe (20)
    reçoit la tension Vsα sur l'axe α du système de coordonnées fixe, le courant Isα sur l'axe α du système de coordonnées fixe, et l'erreur de flux Δsα sur l'axe α du système de coordonnées fixe pour calculer un ratio dλsα/dt de variation du flux sur l'axe α du système de coordonnées par l'utilisation d'une équation dλsα/dt = Vsα - RsIsα + Δsα (Rs : résistance du stator),
    reçoit la tension Vsβ sur l'axe β du système de coordonnées fixe, le courant Isβ sur l'axe β du système de coordonnées fixe, et l'erreur de flux Δsβ sur l'axe β du système de coordonnées fixe pour calculer un ratio dλsβ/dt de variation du flux sur l'axe β du système de coordonnées par l'utilisation d'une équation dλsβ/dt = Vsβ - RsIsβ + Δsβ (Rs : résistance du stator), intègre le ratio dλsα/dt de variation du flux sur l'axe α du système de coordonnées fixe pour délivrer en sortie le flux λsα sur l'axe α, et
    intègre la sortie du ratio dλsβ/dt de variation du flux sur l'axe β du système de coordonnées fixe pour délivrer en sortie le flux λsβ sur l'axe β du système de coordonnées fixe.
  6. Le module d'estimation d'angle de rotation selon la revendication 1, dans lequel l'unité d'estimation d'erreur de flux fixe (30)
    calcule la différence entre la valeur de consigne λsα* de flux sur l'axe α de l'entrée du système de coordonnées fixe venant de l'unité d'estimation de consigne de flux fixe (10) et l'entrée λsα de flux sur l'axe α venant de l'unité d'estimation de flux fixe (20),
    calcule la différence entre la valeur de consigne λsβ* de flux sur l'axe β de l'entrée de système de coordonnées fixe venant de l'unité d'estimation de consigne de flux fixe (10) et l'entrée λsβ de flux sur l'axe β venant de l'unité d'estimation de flux fixe (20),
    reçoit la différence par rapport au flux λsα sur l'axe α pour ajuster un gain et calculer l'erreur Δsα de flux sur l'axe α du système de coordonnées fixe, et
    reçoit la différence par rapport au flux λsβ sur l'axe β pour ajuster un gain et calculer l'erreur Δsβ de flux sur l'axe β du système de coordonnées fixe.
  7. Le module d'estimation d'angle de rotation selon la revendication 1, dans lequel l'unité de calcul de fonction trigonométrique (40) :
    trouve les angles θdq et θαβ par application d'une fonction trigonométrique respectivement au flux tournant (λsd, λsq) et au flux fixe (λsα, λsβ), et
    délivre en sortie l'angle de rotation θ sur la base des angles θdq et θαβ.
  8. Le module d'estimation d'angle de rotation selon la revendication 7, dans lequel l'unité de calcul de fonction trigonométrique (40) :
    reçoit le flux λsd sur l'axe d du système de coordonnées tournant et le flux λsq sur l'axe θ du système de coordonnées tournant venant de l'unité d'estimation de consigne de flux fixe (10) pour délivrer en sortie l'angle θdq de λdq sur la base de l'axe d par utilisation d'une fonction trigonométrique arc tangente,
    reçoit le flux λsα sur l'axe α du système de coordonnées fixe et le flux λsβ sur l'axe β du système de coordonnées fixe venant de l'unité d'estimation de flux fixe (20) pour délivrer en sortie l'angle θαβ de λaβ sur la base de l'axe α par utilisation de la fonction trigonométrique arc tangente, et
    trouve la différence entre les angles θdq et θαβ pour délivrer en sortie l'angle de rotation θ.
  9. Un procédé de mise en oeuvre d'un module d'estimation d'angle de rotation (100) d'un moteur pour le contrôle vectoriel sans capteur d'un PMSM, le procédé de mise en oeuvre comprenant :
    le calcul d'un flux tournant (λsd, λsq) et d'une consigne de flux fixe (λsα*, λsβ*) sur la base du courant (Isα, Isβ) d'un système de coordonnées fixe et d'un angle de rotation (θ) ;
    le calcul d'un flux fixe (λsα, λsβ) sur la base de la tension (Vsα, Vsβ) du système de coordonnées fixe, et du courant (Isα, Isβ) et d'une erreur de flux fixe (Δsα, Asβ) du système de coordonnées fixe, par l'intermédiaire d'une unité d'estimation de flux fixe (20) ;
    l'utilisation de la différence entre la consigne de flux fixe (λsα*, λsβ*) et le flux fixe (λsα, λsβ) pour calculer l'erreur de flux fixe (Δsα, Δsβ) et envoyer les erreurs en retour à l'unité d'estimation de flux fixe (20) ; et
    le calcul de l'angle de rotation (θ) d'une distance dont se déplace un rotor, sur la base du flux tournant (λsd, λsq) et du flux fixe (λsα, λsβ).
  10. Le procédé de mise en oeuvre selon la revendication 9, comprenant en outre le calcul final de l'angle de rotation pour l'envoi d'un angle calculé en retour à l'unité d'estimation de consigne de flux fixe (10).
  11. Le procédé de mise en oeuvre selon la revendication 9, dans lequel le calcul du flux tournant (λsd, λsq) et de la consigne de flux fixe (λsα*, λsβ*) comprend le calcul du flux tournant (λsd, λsq) sur la base du courant (Isα, Isβ) du système de coordonnées fixe, de l'angle de rotation θ, de l'inductance (Ld, Lq) d'un système de coordonnées tournant, et du flux λPM d'un aimant permanent.
  12. Le procédé de mise en oeuvre selon la revendication 11, dans lequel le calcul du flux tournant (λsd, λsq) et de la consigne de flux fixe (λsα*, λsβ*) comprend la compensation de l'angle de rotation θ par utilisation du flux tournant (λsd, λsq) pour calculer la consigne de flux fixe (λsα*, λsβ*).
  13. Le procédé de mise en oeuvre selon la revendication 9, dans lequel le calcul du flux fixe (λsα, λsβ) comprend :
    la réception de la tension Vsα sur l'axe α du système de coordonnées fixe, le courant Isα sur l'axe α du système de coordonnées fixe, et l'erreur de flux Δsα sur l'axe α du système de coordonnées fixe pour calculer un ratio dλsα/dt de variation du flux sur l'axe α du système de coordonnées par l'utilisation d'une équation dλsα/dt = Vsα - RsIsα + Δsα (Rs : résistance du stator),
    la réception de la tension Vsβ sur l'axe β du système de coordonnées fixe, le courant Isβ sur l'axe β du système de coordonnées fixe, et l'erreur de flux Δsβ sur l'axe β du système de coordonnées fixe pour calculer un ratio dΔsβ/dt de variation du flux sur l'axe β du système de coordonnées par l'utilisation d'une équation dλsβ/dt = Vsβ - RsIsβ + Δsβ (Rs : résistance du stator),
    l'intégration du ratio dλsα/dt de variation du flux sur l'axe α du système de coordonnées fixe pour délivrer en sortie le flux λsα sur l'axe α, et
    l'intégration des sorties du ratio dλsβ/dt de variation du flux sur l'axe β du système de coordonnées fixe pour délivrer en sortie le flux λsβ sur l'axe β du système de coordonnées fixe.
  14. Le procédé de mise en oeuvre selon la revendication 9, dans lequel le calcul du flux fixe (λsα, λsβ) comprend :
    le calcul de la différence entre la valeur de consigne λsα* de flux sur l'axe α de l'entrée du système de coordonnées fixe venant de l'unité d'estimation de consigne de flux fixe (10) et l'entrée λsα de flux sur l'axe α venant de l'unité d'estimation de flux fixe (20),
    le calcul de la différence entre la valeur de consigne λsβ* de flux sur l'axe β de l'entrée de système de coordonnées fixe venant de l'unité d'estimation de consigne de flux fixe (10) et l'entrée λsβ de flux sur l'axe β venant de l'unité d'estimation de flux fixe (20),
    la réception de la différence par rapport au flux λsα sur l'axe α pour ajuster un gain et calculer l'erreur Δsα de flux sur l'axe α du système de coordonnées fixe, et
    la réception de la différence par rapport au flux λsβ sur l'axe β pour ajuster un gain et calculer l'erreur Δsβ de flux sur l'axe β du système de coordonnées fixe.
  15. Le procédé de mise en oeuvre selon la revendication 9, dans lequel le calcul de l'angle de rotation θ comprend :
    l'obtention des angles θdq et θαβ par application d'une fonction trigonométrique respectivement au flux tournant (λsd, λsq) et au flux fixe (λsα, λsβ), et
    la délivrance en sortie de l'angle de rotation θ sur la base des angles (θdq, θαβ).
EP15163779.0A 2014-04-29 2015-04-16 Module d'estimation d'angle de rotation pour commande vectorielle sans capteur de pmsm Not-in-force EP2940859B1 (fr)

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CN105048919B (zh) 2018-01-30
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